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Alternative TitleResearch on Formation Initialization Control for Elliptic Reference Orbit
雷博持; 郑建华; 李明涛
Source Publication空间科学学报
Keyword椭圆参考轨道 构型初始化 三迹向脉冲 四迹向脉冲
Other AbstractFormation initialization for elliptic reference orbit is studied in this paper, and three formation initialization strategies for planner formation configuration are derived. Firstly, two impulsive initialization strategy is derived using the state transition matrix. Secondly, three and four in-track impulsive initialization strategies are studied using the Gauss perturbation equations with the principle of minimal fuel consumption. Finally, numerical simulations of three initialization strategies are carried out, and the sequence quadratic programming and genetic algorithm are proposed to optimize the numerical results. Simulation results show that three in-track impulsive initialization strategy requires about 41% less velocity increment compared with two impulsive initialization strategy, and four in-track impulsive initialization strategy requires almost equal velocity increment compared with three in-track impulsive initialization strategy.
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Cited Times:2[CSCD]   [CSCD Record]
Document Type期刊论文
Recommended Citation
GB/T 7714
雷博持,郑建华,李明涛. 椭圆轨道编队构型的初始化控制研究[J]. 空间科学学报,2015,35(1):86-93.
APA 雷博持,郑建华,&李明涛.(2015).椭圆轨道编队构型的初始化控制研究.空间科学学报,35(1),86-93.
MLA 雷博持,et al."椭圆轨道编队构型的初始化控制研究".空间科学学报 35.1(2015):86-93.
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